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Patent # Description
2016/0347499 PAINT CONTAINER
A paint container comprises a plurality of walls arranged circumferentially to form a hollow enclosure with a bore within which a volume of paint may be...
2016/0347498 REINFORCED TRAY STACK CONTAINER
Various box embodiments are disclosed. In one aspect, a box is provided that includes a container. The container has a bottom panel, a front panel, a first...
2016/0347497 Paperboard Carton
A paperboard carton is formed by interconnecting a main body piece, folded to establish at least a bottom wall and first and second spaced side panels, with...
2016/0347496 REUSABLE PRODUCE CONTAINERS AND RELATED METHODS
Embodiments of foldable containers, such as foldable produce containers, and related planar sheets and methods. In some embodiments, a substantially planar...
2016/0347495 T or L-SLOT DIVIDERS WITH INTERFERENCE SECTION FOR USE WITH INDUSTRIAL BINS
The present invention provides a bin having an interference fit divider, including a bin having a base, a front wall, a rear wall and opposed side walls; at...
2016/0347494 COMPOSTABLE PREFORM
An injection molded preform is presented. The injection molded perform includes a body, the body having a finish portion, a transition portion in mechanical...
2016/0347493 BOTTLING AND LABELING MACHINE
A servo controlled labeling apparatus, comprises a conveyor for supplying a plurality of articles through a conveyor guide, an active star wheel having a...
2016/0347492 Packaging Method To Enable Re-Sterilization Of Medical Device
A method of packaging pre-filled medical devices is disclosed. The method comprises producing a packaging having a front panel and a back panel defining a...
2016/0347491 FILM SEALING MECHANISM
To allow a tubular film having a large opening diameter to be heat-sealed with a short length heater by a function (film width reduction function) that can...
2016/0347490 APPARATUS AND METHOD FOR FILLING CONTAINERS
A filling apparatus for filling containers, and a method of operation, are disclosed, whereby a plurality of container carriers are movable along an upper...
2016/0347489 Method and Apparatus for Vacuum Packaging a Product
A method and apparatus for vacuum packaging a product. According to one embodiment a film tube is generated, and, in the film tube a product (P) is introduced...
2016/0347488 Packaging System
A method of loading articles in cartons. The method can comprise moving a carton in a generally flat configuration in a downstream direction with a carton...
2016/0347487 BAG-PACKING SYSTEM
A box-packing system having a first conveyor, a first robot that applies suction, holds, and transports a package, and a control device. The package includes...
2016/0347486 METHOD FOR LOADING A 3D FLEXIBLE POUCH TO BE FILLED, SYSTEM FOR LOADING AND STORING THIS FLEXIBLE POUCH AND...
A support device (20), mounted on an upper edge of a container (3), includes lifting elements that define a support surface (22) which extends transversely...
2016/0347485 THREE CIRCUIT FILL SYSTEM FOR BLOW FILL SEAL CONTAINERS
A system for filling a blow-fill-seal (BFS) container is provided. The system includes a first fluid circuit constructed to selectively deliver a purge fluid...
2016/0347484 UNIT AND METHOD FOR FILLING CONTAINERS FORMING SINGLE-USE CAPSULES FOR EXTRACTION OR INFUSION BEVERAGES
Described is a unit for filling containers (2) forming single-use capsules (3) with a dose (33) of product for extraction or infusion beverages, comprising: a...
2016/0347483 UNIT AND METHOD FOR RELEASING PRODUCT FOR EXTRACTION OR INFUSION BEVERAGES IN CONTAINERS FORMING SINGLE-USE...
Described is a unit for releasing product for extraction or infusion beverages in containers (2) forming single-use capsules (3) comprising: at least one seat...
2016/0347482 SYSTEMS AND METHODS FOR ESTIMATING PARAMETERS OF A SPACECRAFT BASED ON EMISSION FROM AN ATOMIC OR MOLECULAR...
A parameter of an actual spacecraft can be estimated based on a spectroscopic image of an emission from an atomic or molecular product of an interaction...
2016/0347481 Energy Absorbing Restraint Device
An energy absorbing restraint device for a clamp system is disclosed. The clamp system can include a releasable clamp having first and second ends, a securing...
2016/0347480 AIRCRAFT CAPABLE OF PASSING FROM THE AERIAL DOMAIN TO THE SPATIAL DOMAIN AND METHOD FOR AUTOMATICALLY ADAPTING...
An aircraft is capable of passing from the aerial domain to the spatial domain and method for automatically adapting the configuration of same. An additional...
2016/0347479 MULTIPLE POWER ASSURANCE CHECK PROCEDURE FOR AIRCRAFT WITH AN ENGINE INLET BARRIER FILTER INSTALLED
A method of conducting an engine power assurance check includes performing a first engine power assurance check wherein the first engine power assurance check...
2016/0347478 TEMPORARILY-INSTALLED AIRCRAFT OBSERVER DOOR PLUG, CHAIR, SONOTUBE EJECTION AND CONTROL SYSTEM
In one embodiment, a non-dedicated, temporarily-installed, aircraft observer bubble door, chair, sonotube ejection system, mission electronics LRU rack and...
2016/0347477 ELECTRIC UNMANNED AERIAL VEHICLE LAUNCHER
Embodiments of the present invention provide improvements to UAV launching systems. The disclosed launching system eliminates the use of hydraulic fluid and...
2016/0347476 SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE
An unmanned aerial vehicle launch tube that has at least one layer of prepeg substrate disposed about an aperture to form a tube, a sabot disposed in an...
2016/0347475 HELICOPTER DOLLY
A helicopter dolly includes a platform defining a helicopter landing area, a plurality of rollers connected to the platform such that a vertical clearance is...
2016/0347474 LIGHTING DEVICE FOR AIRCRAFT ALLOWING THE INTEGRATION OF ADDITIONAL FUNCTIONS AT ITS CENTER
A Light Emitting Diode (LED) light for an aircraft includes a hollow cylindrical body, a plurality of LEDs mounted in the hollow body, and at least one...
2016/0347473 INTEGRATION OF BRAKING ACTION INFORMATION WITH FLIGHT DECK RUNWAY FUNCTIONS
Flight deck systems are provided for integrating braking action information with flight deck runway functions. In one embodiment, the flight deck system...
2016/0347472 WEARABLE ELECTRONIC DISPLAY AND METHOD FOR DISPLAYING INFORMATION TO A PILOT
A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures,...
2016/0347471 MODIFYING THE APPEARANCE OF AN UPLINK MESSAGE WHEN THE UPLINK MESSAGE IS AFFECTED BY A FLIGHT INFORMATION MESSAGE
An avionics display system is provided that modifies the appearance of an uplink message when the uplink message is affected by a flight information message....
2016/0347470 VEHICLE HEALTH MANAGEMENT SYSTEMS AND METHODS
A method includes receiving first vehicle data from a sensor on a vehicle at one or more processors executing a first software module. The method includes...
2016/0347469 Aircraft Recovery Control
Despite pilot training and current safety systems, aircraft accidents continue to occur. It is recognized herein that existing approaches to preventing...
2016/0347468 METHOD AND DEVICE FOR ACTIVATING THE DISPLAY OF AT LEAST ONE STALL MARGIN INDICATOR OF AN AIRCRAFT
An activation device comprising a computation unit configured to compute a stall margin of the aircraft, an information reception unit configured to receive...
2016/0347467 METHOD OF DETERMINING THE LONGITUDINAL AIR SPEED AND THE LONGITUDINAL GROUND SPEED OF A ROTARY WING AIRCRAFT...
A method of determining the longitudinal air speed V.sub.airX and the longitudinal ground speed V.sub.solX of a rotary wing aircraft depending on the exposure...
2016/0347466 PIEZOELECTRICALLY-CONTROLLED FUEL DELIVERY SYSTEM
A fuel delivery system is provided for filling a fuel tank with a prescribed volume of fuel. The delivery system includes a fuel tank, a ...
2016/0347465 POSITIVE LOCK LATCHING MECHANISM
An apparatus and method according to one or more embodiments are provided for a latching mechanism. The latching mechanism may be implemented, for example, as...
2016/0347464 Load Bearing Element And A Method For Manufacturing A Load Bearing Element
A load bearing element for attachment of a heat generating unit to a heat sensitive supporting structure, wherein said load bearing element includes at least...
2016/0347463 ADAPTIVE AIRCRAFT ENGINE AND AIRCRAFT HAVING AN ADAPTIVE ENGINE
An adaptive aircraft engine including a first, inner bypass duct inside a core engine of the aircraft engine and a second, outer bypass duct at least partially...
2016/0347462 UNMANNED AERIAL VEHICLE RECOVERY SYSTEM
An unmanned aerial vehicle includes a closely integrated emergency recovery and operation systems for an unmanned aerial vehicle with built-in levels of...
2016/0347461 DEICER BOOTS HAVING ELASTOMER FIBERS WITH ALIGNED CARBON ALLOTROPE MATERIALS
A deicer boot includes an aircraft structure and an outer layer. The outer layer includes a plurality of elastomer fibers and a carbon allotrope material. The...
2016/0347460 POLYETHER URETHANE DEICER BOOTS
A deicer includes an aircraft structure and an outer layer with a sheet having a brittle point lower than -40.degree. C. (-40.degree. F.). The sheet includes a...
2016/0347459 NACELLES FOR AIRCRAFT ENGINES WITH DE-ICING SYSTEMS USING A TWO-PHASE FLUID
Nacelles are provided having a tubular casing, open at its opposite axial ends, with an inner wall and an outer wall which are connected to each other at the...
2016/0347458 DEICER BOOTS HAVING DIFFERENT ELASTOMER FIBERS
A deicer boot includes a plurality of first elastomer fibers and a first carbon allotrope material selected from the group consisting of carbon nanotubes,...
2016/0347457 SUPPLY OF AIR TO AN AIR-CONDITIONING CIRCUIT OF AN AIRCRAFT CABIN FROM ITS TURBOPROP ENGINE
An aircraft turboprop engine has at least a low-pressure body and a high-pressure body. The low-pressure body drives a propeller by means of a first gearbox....
2016/0347456 AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
An environmental control system (ECS) pack is provided including a primary heat exchanger and a secondary heat exchanger. An air cycle machine is arranged in...
2016/0347455 ARMREST PIVOT GUARD
An armrest assembly for a seat including a static frame member, an armrest pivotally attached at one end to the static frame member, and an armrest pivot guard...
2016/0347454 REMOVABLE SEAT DIVIDER FOR PLACEMENT IN A SEAT
Disclosed is a removable seat divider for placement in a seat. The removable seat divider includes a vertical structure configured to be placed on the seat...
2016/0347453 ENERGY-HARVESTING-BASED CONTROL AND COMMUNICATION FOR A CABIN SERVICES SYSTEM
A passenger control unit is provided that may include a push-button, power assembly, and control and communication circuitry. The push-button may be for...
2016/0347452 AUTOMOTIVE DRONE DEPLOYMENT SYSTEM
This disclosure generally relates to an automotive drone deployment system that includes at least a vehicle and a deployable drone that is configured to attach...
2016/0347451 METHODS FOR OPERATING AN AIR VEHICLE
Methods are provided for operating an air vehicle having fixed wings. Such methods include the step of providing an operating map of angle of attack associated...
2016/0347450 SYSTEM FOR RECHARGING REMOTELY CONTROLLED AERIAL VEHICLE, CHARGING STATION AND RECHARGEABLE REMOTELY CONTROLLED...
A system including an aerial vehicle having an airframe and a power source onboard the aerial vehicle, wherein the aerial vehicle includes a landing gear...
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